Effect on tail-fin span on stability and control characteristics of a canard-controlled missile at supersonic Mach numbers
Read Online
Share

Effect on tail-fin span on stability and control characteristics of a canard-controlled missile at supersonic Mach numbers by A. B. Blair

  • 882 Want to read
  • ยท
  • 76 Currently reading

Published by National Aeronautics and Space Administration, Scientific and Technical Information Branch, For sale by the National Technical Information Service] in Washington, D.C, [Springfield, Va .
Written in English

Subjects:

  • Guided missiles -- Wings.,
  • Airplanes -- Wings, Canard.,
  • Aerodynamics, Supersonic.

Book details:

Edition Notes

StatementA.B. Blair, Jr., Jerry M. Allen, and Gloria Hernandez.
SeriesNASA technical paper -- 2157.
ContributionsAllen, Jerry M., Hernandez, Gloria., United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
The Physical Object
Pagination83 p. :
Number of Pages83
ID Numbers
Open LibraryOL17553098M

Download Effect on tail-fin span on stability and control characteristics of a canard-controlled missile at supersonic Mach numbers

PDF EPUB FB2 MOBI RTF